US4156614A - Alumina-based ceramics for core materials - Google Patents

Alumina-based ceramics for core materials Download PDF

Info

Publication number
US4156614A
US4156614A US05/839,990 US83999077A US4156614A US 4156614 A US4156614 A US 4156614A US 83999077 A US83999077 A US 83999077A US 4156614 A US4156614 A US 4156614A
Authority
US
United States
Prior art keywords
alumina
ceramic
fired
core
ceramic material
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US05/839,990
Other languages
English (en)
Inventor
Charles D. Greskovich
Robert C. DeVries
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US05/839,990 priority Critical patent/US4156614A/en
Priority to JP9416878A priority patent/JPS5455013A/ja
Priority to EP78101012A priority patent/EP0001434A1/en
Priority to IT28255/78A priority patent/IT1099621B/it
Priority to NO783375A priority patent/NO783375L/no
Application granted granted Critical
Publication of US4156614A publication Critical patent/US4156614A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/10Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
    • C04B35/111Fine ceramics
    • C04B35/113Fine ceramics based on beta-aluminium oxide
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C1/00Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/10Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
    • C04B35/101Refractories from grain sized mixtures

Definitions

  • This invention relates to materials suitable for making cores for casting directionally solidified eutectic and superalloy materials.
  • Jet engines are a multi-million dollar business. The maximum operating temperature of these engines must be increased to attain higher efficiencies. Higher operating temperatures require the fabrication of new alloys with high temperature strength, toughness and corrosion resistance.
  • the most promising method of fabricating the turbine blade components with improved high temperature properties is by directional solidification (DS).
  • DS directional solidification
  • the rate of production of blades by the DS process is partly governed by the liquidus temperature which should be as high as possible.
  • the liquidus temperature of many of the promising alloy compositions being explored at this time is greater than 1500° C. and reaches nearly 1800° C. or higher.
  • the alloy is solidified around a ceramic core material which is subsequently leached away, leaving behind the proper air cooling cavities in the blade.
  • fused silica is the standard core material used at temperatures up to about 1550° C. without deleterious reaction with many of the alloy compositions.
  • silica cores are severely attached by one or more of the most reactive elements (A1, Hf, C) of the alloy. Consequently, silica cores cannot be used at the high temperatures required to directionally solidify the alloy. MgO and Y 2 O 3 cores are found to react only slightly with the aluminum in the alloy during DS at temperatures near 1800° C., but both materials have relatively poor leachabilities.
  • leachability and nonreactivity with the alloy up to 1800° C. are the two primary characteristics of the core material, other desirable characteristics are that it (1) be economical, (2) not undergo more than an overall dimensional change of ⁇ 2-4%, (3) have a porosity of from about 25% to about 60% to aid degassing during DS and increase the rate of leachability, (4) exhibit a modulus of rupture of only about 100 psi so that good crushability of the core occurs after the metal is cast, and (5) have good thermal shock resistance.
  • Another object of this invention is to provide a new and improved material composition for making ceramic cores which is also economical for use in casting directionally solidified eutectic alloys and superalloy materials.
  • a further object of this invention is to provide a new and improved material composition for making ceramic cores having increased porosity, leachability and crushability characteristics.
  • a fired ceramic compact suitable for use in a core in the casting and directional solidification of eutectic alloys and superalloy materials.
  • the ceramic material is an alumina-based material such as ⁇ -alumina, Na 2 O . 9A1 2 O 3 - Na 2 O . 11Al 2 O 3 , and other choice candidate materials such as CaO . 6Al 2 O 3 , SrO . 6A1 2 O 3 and BaO . 6Al 2 O 3 .
  • the ceramic material after firing is characterized by an interconnected network of porosity and solid phase.
  • the density of the fired compact is from about 40% to about 75%.
  • a desirable material composition can also be produced by admixing up to about 40 parts by weight of pure alumina to each of the alumina-based ceramic compounds and form in situ the interconnected network in which may be found a dispersion of particles of alumina within a matrix of alumina-based compounds.
  • Cores made of alumina-based ceramics of this invention are easily removed from the cast metal by autoclave leaching techniques embodying solutions of KOH or NaOH.
  • the ⁇ -aluminates, Na 2 O ⁇ 9Al 2 O 3 - Na 2 O ⁇ 11Al 2 O 3 are desirable for making the ceramic cores because of their excellent leaching characteristics.
  • Alumina-based compounds such as Na 2 O ⁇ 9Al 2 O 3 - Na 2 O ⁇ 11Al 2 O 3 , CaO ⁇ 6Al 2 O 3 , SrO ⁇ 6Al 2 O 3 and BaO . 6Al 2 O 3 have been discovered to be suitable materials for use in making cores for use in casting directionally solidified eutectic alloy and superalloy materials. All of these materials have a minimum temperature at which a liquid phase forms between the compound and alumina (Al.sub. 2 O 3 ) which is greater than 1800° C. which is the predicted maximum temperature that will be imposed upon the ceramic core material during directional solidification.
  • the alumina-based compounds may comprise at least in part the ceramic material composition used in preparing a ceramic core from the composition.
  • the material composition may consist essentially of 100 parts by weight of an individual alumina-based compound. Alternately the composition may comprise a two phase mixture of from about 60 parts by weight to 100 parts by weight of the alumina-based compounds, balance alumina.
  • a continuous phase of the alumina-based ceramic compound is formed in situ which provides either an interconnected network of solid and porous phases or a dispersion of particles of alumina within a porous matrix of alumina-based compounds.
  • Fired compacts of any of these material compositions when employed as cores in the casting and directional solidification of eutectic and superalloy materials, are easily removed therefrom by a caustic autoclave processing technique. Removal is achieved by leaching away the interconnected network of the alumina-based ceramic compound with a caustic agent of either a KOH or a NaOH solution.
  • Another particular feature of material compositions embodying two phase ceramic cores is that the activity of the alumina in the core is nearly equal to that of pure alumina.
  • the activity of the other oxide constituent in the phase mixture such, for example as Na 2 O, is considerably reduced so as to decrease its volatility to decrease its possible reactivity with the superalloy melt.
  • Cores made from material compositions including one or more of these sodium aluminates are leachable in a 20% KOH or NaOH aqueous solution at from 200° C. to 350° C. in an autoclave.
  • the process is economical and fairly fast, the leaching rate being on the order of from 0.5 to 1.0 centimeters per hour.
  • the material composition for core making is prepared by mixing the materials together mechanically. A sufficient amount of the material composition, with or without a binder material admixed therein, is placed in a mold and pressed to a green compact having a desired configuration. The green compact is fired at a temperature of from 1600° C. to 1800° C. to form the core whose material is characterized by a continuous phase of alumina-based ceramic compound formed in situ by sintering.
  • the material structure is characterized by either an interconnected network of solid and porous phases or particles of alumina within a porous matrix of alumina-based compounds.
  • the density of the fired compact varies with the particle size of the materials employed. For a range of particle size of from about 1 micron to about 50 microns, the density of the fired compact ranges from about 40 percent to about 75 percent.
  • a core 8 cm + 0.6 cm was made of substantially 100 parts by weight ⁇ -alumina material (Na 2 O ⁇ 9A1 2 O 3 ).
  • the average particle size of the material used was about 35 microns for a particle size distribution ranging between 5 and 50 microns.
  • the compact was formed at a pressure of 10,000 psi and fired at 1800° C. ⁇ 10° C. to sinter the compact for ease of handling.
  • the density of the sintered rod was 55 percent.
  • a melt of NiTaC-13 alloy was prepared, cast about the rod and directionally solidified thereabout at a temperature of 1675° C. ⁇ 25° C. for 20 hours in a controlled atmosphere of 10% CO by volume of argon gas.
  • the alloy composition, as cast was as follows:

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Mold Materials And Core Materials (AREA)
  • Porous Artificial Stone Or Porous Ceramic Products (AREA)
  • Ceramic Products (AREA)
US05/839,990 1977-10-06 1977-10-06 Alumina-based ceramics for core materials Expired - Lifetime US4156614A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
US05/839,990 US4156614A (en) 1977-10-06 1977-10-06 Alumina-based ceramics for core materials
JP9416878A JPS5455013A (en) 1977-10-06 1978-08-03 Ceramic based on coreemateriallgrade alumina
EP78101012A EP0001434A1 (en) 1977-10-06 1978-09-28 Alumina-based ceramics for core materials
IT28255/78A IT1099621B (it) 1977-10-06 1978-09-29 Ceramiche basate su allumina per materiali di anima da fonderia
NO783375A NO783375L (no) 1977-10-06 1978-10-05 Keramisk materiale paa basis av aluminiumoxyd

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/839,990 US4156614A (en) 1977-10-06 1977-10-06 Alumina-based ceramics for core materials

Publications (1)

Publication Number Publication Date
US4156614A true US4156614A (en) 1979-05-29

Family

ID=25281174

Family Applications (1)

Application Number Title Priority Date Filing Date
US05/839,990 Expired - Lifetime US4156614A (en) 1977-10-06 1977-10-06 Alumina-based ceramics for core materials

Country Status (5)

Country Link
US (1) US4156614A (it)
EP (1) EP0001434A1 (it)
JP (1) JPS5455013A (it)
IT (1) IT1099621B (it)
NO (1) NO783375L (it)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4480681A (en) * 1982-08-30 1984-11-06 Doulton Industrial Products Limited Refractory mould body and method of casting using the mould body
US4837187A (en) * 1987-06-04 1989-06-06 Howmet Corporation Alumina-based core containing yttria
US4836268A (en) * 1987-01-17 1989-06-06 Rolls-Royce Plc Method of enhancing the leaching rate of a given material
WO1989005204A1 (en) * 1987-12-08 1989-06-15 Harri Sahari Method for preparation of moulds and cores used in the casting of metals
US5129998A (en) * 1991-05-20 1992-07-14 Reynolds Metals Company Refractory hard metal shapes for aluminum production
US5336645A (en) * 1993-09-27 1994-08-09 Corning Incorporated Soluble, cellulated mold and foamable mixture
US5409871A (en) * 1993-11-02 1995-04-25 Pcc Airfoils, Inc. Ceramic material for use in casting reactive metals
US5545003A (en) * 1992-02-18 1996-08-13 Allison Engine Company, Inc Single-cast, high-temperature thin wall gas turbine component
US5552356A (en) * 1994-07-11 1996-09-03 Bayer Ag Boron subphosphide/aluminum oxide composite materials, processes for the production thereof and use thereof
US5810552A (en) * 1992-02-18 1998-09-22 Allison Engine Company, Inc. Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same
US6494250B1 (en) 2001-05-14 2002-12-17 Howmet Research Corporation Impregnated alumina-based core and method
US20050269055A1 (en) * 1998-11-20 2005-12-08 Frasier Donald J Method and apparatus for production of a cast component
US20060243421A1 (en) * 2005-04-29 2006-11-02 United States Of America, Represented By Secretary Of The U.S. Army Soluble casting core for metal matrix composite components and method of producing thereof
US20080135204A1 (en) * 1998-11-20 2008-06-12 Frasier Donald J Method and apparatus for production of a cast component
US10364189B2 (en) 2017-05-04 2019-07-30 General Electric Company Methods for forming ceramic cores

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2042951B (en) * 1978-11-08 1982-08-04 Rolls Royce Investment casting core
JPS62153158A (ja) * 1985-08-30 1987-07-08 東洋シーシーアイ株式会社 耐熱性触媒又は触媒担体及びその製造方法
US4771028A (en) * 1985-08-30 1988-09-13 Catalysts And Chemicals Inc. Heat resistant composition and method of producing the same
JPS63242917A (ja) * 1987-03-27 1988-10-07 Agency Of Ind Science & Technol 耐熱性アルミナ複合酸化物の製造方法
GB8925289D0 (en) * 1989-11-09 1989-12-28 Lilliwyte Sa Method of making analogues of beta"-alumina
US5458868A (en) * 1989-11-09 1995-10-17 Lilliwyte Societe Anonyme Method of making analogues of β-alumina
US20160175923A1 (en) * 2012-04-09 2016-06-23 General Electric Company Composite core for casting processes, and processes of making and using the same
JP6366555B2 (ja) * 2015-09-24 2018-08-01 日本特殊陶業株式会社 スパークプラグ

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB618248A (en) * 1945-04-10 1949-02-18 Corning Glass Works Cast refractory products
US3078173A (en) * 1960-11-08 1963-02-19 Harbison Walker Refractories Aluminum melting furnace refractory
US3312558A (en) * 1966-05-17 1967-04-04 Jr Eldon D Miller Calcium hexaluminate articles
US3643728A (en) * 1970-07-08 1972-02-22 United Aircraft Corp Process of casting nickel base alloys using water-soluble calcia cores
JPS4920365A (it) * 1972-05-20 1974-02-22
US3901733A (en) * 1974-10-07 1975-08-26 Trw Inc Thin film solid electrolyte structures and process of making same
US4052538A (en) * 1976-04-19 1977-10-04 General Motors Corporation Method of making sodium beta-alumina powder and sintered articles
US4068048A (en) * 1975-03-20 1978-01-10 Compagnie Generale D'electricite S.A. Method for preparing alkaline beta alumina parts
US4073662A (en) * 1977-03-09 1978-02-14 General Electric Company Method for removing a magnesia doped alumina core material

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR484314A (fr) * 1916-02-02 1917-09-25 Edward Irwing Braddock Perfectionnements aux pointes ou clous fabriqués avec du fil métallique
DE1257050B (de) * 1959-06-23 1967-12-21 Harbison Walker Refractories Gebrannter, feuerfester Formkoerper fuer die Auskleidung von metallurgischen Gefaessen, in denen fluessiges Aluminium gehandhabt wird
GB1185725A (en) * 1967-11-03 1970-03-25 Ass Elect Ind Beta-Alumina Polycrystalline Ceramics
GB1287571A (en) * 1968-08-05 1972-08-31 English Electric Co Ltd Ceramic materials
BE758568A (fr) * 1969-11-10 1971-05-06 Aluminum Co Of America Perfectionnement du procede de production de l'alumine beta
BE791380A (fr) * 1972-01-19 1973-03-01 Buckbee Mears Co Produits ceramiques et compositions ceramiques
CA1065580A (en) * 1975-05-02 1979-11-06 Donald Pearlman Methods for producing beta-alumina composites

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB618248A (en) * 1945-04-10 1949-02-18 Corning Glass Works Cast refractory products
US3078173A (en) * 1960-11-08 1963-02-19 Harbison Walker Refractories Aluminum melting furnace refractory
US3312558A (en) * 1966-05-17 1967-04-04 Jr Eldon D Miller Calcium hexaluminate articles
US3643728A (en) * 1970-07-08 1972-02-22 United Aircraft Corp Process of casting nickel base alloys using water-soluble calcia cores
JPS4920365A (it) * 1972-05-20 1974-02-22
US3901733A (en) * 1974-10-07 1975-08-26 Trw Inc Thin film solid electrolyte structures and process of making same
US4068048A (en) * 1975-03-20 1978-01-10 Compagnie Generale D'electricite S.A. Method for preparing alkaline beta alumina parts
US4052538A (en) * 1976-04-19 1977-10-04 General Motors Corporation Method of making sodium beta-alumina powder and sintered articles
US4073662A (en) * 1977-03-09 1978-02-14 General Electric Company Method for removing a magnesia doped alumina core material

Cited By (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4480681A (en) * 1982-08-30 1984-11-06 Doulton Industrial Products Limited Refractory mould body and method of casting using the mould body
US4836268A (en) * 1987-01-17 1989-06-06 Rolls-Royce Plc Method of enhancing the leaching rate of a given material
US4837187A (en) * 1987-06-04 1989-06-06 Howmet Corporation Alumina-based core containing yttria
WO1989005204A1 (en) * 1987-12-08 1989-06-15 Harri Sahari Method for preparation of moulds and cores used in the casting of metals
GB2230269A (en) * 1987-12-08 1990-10-17 Harri Sahari Method for preparation of moulds and cores used in the casting of metals
GB2230269B (en) * 1987-12-08 1991-05-15 Harri Sahari Method for preparation of moulds and cores used in the casting of metals
US5129998A (en) * 1991-05-20 1992-07-14 Reynolds Metals Company Refractory hard metal shapes for aluminum production
US5924483A (en) * 1992-02-18 1999-07-20 Allison Engine Company, Inc. Single-cast, high-temperature thin wall structures having a high conductivity member connecting the walls and methods of making the same
US6255000B1 (en) 1992-02-18 2001-07-03 Allison Engine Company, Inc. Single-cast, high-temperature, thin wall structures
US5545003A (en) * 1992-02-18 1996-08-13 Allison Engine Company, Inc Single-cast, high-temperature thin wall gas turbine component
US6244327B1 (en) 1992-02-18 2001-06-12 Allison Engine Company, Inc. Method of making single-cast, high-temperature thin wall structures having a high thermal conductivity member connecting the walls
US6071363A (en) * 1992-02-18 2000-06-06 Allison Engine Company, Inc. Single-cast, high-temperature, thin wall structures and methods of making the same
US5641014A (en) * 1992-02-18 1997-06-24 Allison Engine Company Method and apparatus for producing cast structures
US5810552A (en) * 1992-02-18 1998-09-22 Allison Engine Company, Inc. Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same
US5336645A (en) * 1993-09-27 1994-08-09 Corning Incorporated Soluble, cellulated mold and foamable mixture
US5580837A (en) * 1993-11-02 1996-12-03 Pcc Airfoils, Inc. Ceramic material for use in casting reactive metals
US5409871A (en) * 1993-11-02 1995-04-25 Pcc Airfoils, Inc. Ceramic material for use in casting reactive metals
US5552356A (en) * 1994-07-11 1996-09-03 Bayer Ag Boron subphosphide/aluminum oxide composite materials, processes for the production thereof and use thereof
US20080142186A1 (en) * 1998-11-20 2008-06-19 Frasier Donald J Method and apparatus for production of a cast component
US20050269055A1 (en) * 1998-11-20 2005-12-08 Frasier Donald J Method and apparatus for production of a cast component
US20080135204A1 (en) * 1998-11-20 2008-06-12 Frasier Donald J Method and apparatus for production of a cast component
US20080149295A1 (en) * 1998-11-20 2008-06-26 Frasier Donald J Method and apparatus for production of a cast component
US7779890B2 (en) 1998-11-20 2010-08-24 Rolls-Royce Corporation Method and apparatus for production of a cast component
US8082976B2 (en) 1998-11-20 2011-12-27 Rolls-Royce Corporation Method and apparatus for production of a cast component
US8844607B2 (en) 1998-11-20 2014-09-30 Rolls-Royce Corporation Method and apparatus for production of a cast component
US8851152B2 (en) 1998-11-20 2014-10-07 Rolls-Royce Corporation Method and apparatus for production of a cast component
US8851151B2 (en) 1998-11-20 2014-10-07 Rolls-Royce Corporation Method and apparatus for production of a cast component
US6494250B1 (en) 2001-05-14 2002-12-17 Howmet Research Corporation Impregnated alumina-based core and method
US20060243421A1 (en) * 2005-04-29 2006-11-02 United States Of America, Represented By Secretary Of The U.S. Army Soluble casting core for metal matrix composite components and method of producing thereof
US20070131374A1 (en) * 2005-04-29 2007-06-14 U.S. Government, Represented By Secretary Of The Army Soluble Casting Core For Metal Matrix Composite Components and Method of Producing Thereof
US10364189B2 (en) 2017-05-04 2019-07-30 General Electric Company Methods for forming ceramic cores

Also Published As

Publication number Publication date
NO783375L (no) 1979-04-09
JPS5455013A (en) 1979-05-01
IT1099621B (it) 1985-09-18
IT7828255A0 (it) 1978-09-29
EP0001434A1 (en) 1979-04-18

Similar Documents

Publication Publication Date Title
US4156614A (en) Alumina-based ceramics for core materials
US4141781A (en) Method for rapid removal of cores made of βAl2 O3 from directionally solidified eutectic and superalloy and superalloy materials
US4837187A (en) Alumina-based core containing yttria
EP0204674B1 (en) Casting of reactive metals into ceramic molds
EP0252862B1 (en) Ceramic shell mold facecoat and core coating systems for investment casting of reactive metals
US4164424A (en) Alumina core having a high degree of porosity and crushability characteristics
EP0914883B1 (en) Erbia-bearing core
US4097292A (en) Core and mold materials and directional solidification of advanced superalloy materials
US4187266A (en) Process for making a ceramic article having a dense integral outer barrier layer and a high degree of porosity and crushability characteristics
US4073662A (en) Method for removing a magnesia doped alumina core material
US5335717A (en) Oxidation resistant superalloy castings
US3981352A (en) Metal casting mold with bonded particle filter
US4086311A (en) Methods for increasing the crushability characteristics of cores for casting advanced superalloy materials
GB1602030A (en) Ceramic cores for investment casting
US4097291A (en) Core and mold materials for directional solidification of advanced superalloy materials
US4191721A (en) Making ceramic articles having a high degree of porosity and crushability characteristics
EP0280874A1 (en) Method for the manufacture of an object from powdered material by isostatic pressing
US4240828A (en) Method for minimizing the formation of a metal-ceramic layer during casting of superalloy materials
EP0061479B1 (en) Removing refractory material from components
US4162918A (en) Rare earth metal doped directionally solidified eutectic alloy and superalloy materials
US4102689A (en) Magnesia doped alumina core material
US4188450A (en) Shell investment molds embodying a metastable mullite phase in its physical structure
US7845390B2 (en) Hafnia-modified rare-earth metal-based ceramic bodies and casting processes performed therewith
EP0179649A2 (en) Ceramic materials
US4221594A (en) Material composition for fired ceramic articles having a high degree of porosity and crushability characteristics